Pulse radar and components therefor

Claim 3

The apparatus as recited in claim 1 wherein the rotating means rotates the electric fields of the first and the second beams of RF energy 45 degrees.

Claim 4

The apparatus as recited in claim 2 further comprising second means, disposed in the path of propagation of the first and the second beams of RF energy, for reflecting the path of the first and the second beam of RF energy and for passing a third beam of RF energy through said second means.

Claim 5

The apparatus as recited in claim 3 further comprising means, disposed in the path of propagation of the first, the second and the third beams of RF energy, for changing the second and the third beams of RF energy from circular polarization to linear polarization and for changing the first beam of RF energy from linear polarization to circular polarization.

Claim 6

The apparatus as recited in claim 4 further comprising a plurality of lens disposed in the path of the first beam of RF energy.

Claim 9

The apparatus as recited in claim 6 further comprising a second polarization grid in the path of the rotated beam of RF energy, the second polarization grid being inclined at an angle of 45° to the axis of the rotated beam and having parallel conductive strips disposed in parallel with the direction of polarization of the rotated beam of RF energy to reflect the rotated beam.

Claim 10

The apparatus as recited in claim 7 further comprising a quarter wave plate disposed in the path of the reflected rotated beam of RF energy to change the polarization of the reflected rotated beam to circularly polarized.

Claim 11

The apparatus as recited in claim 8 further comprising a plurality of lens disposed in the path of the beam of RF energy.

Claim 12

A radar seeker for a missile comprising: (a) means, responsive to a first beam of radio frequency (RF) energy having an electric field and a first path of propagation and responsive to a second beam of RF energy having an electric field orthogonal to the electric field of the first beam of RF energy and a second path of propagation, for passing the first beam of RF energy through said means and for reflecting the second beam of RF energy; and (b) means, disposed in the path of the first and the second beam of RF energy, for rotating the electric field of the first beam in a direction by 45° and for rotating the electric field of the second beam of RF energy in a similar direction by 45°.

Claim 13

A radar seeker for a missile comprising: (a) means, responsive to a first beam of radio frequency (RF) energy having an electric field and a first path of propagation and responsive to a second beam of RF energy having an electric field orthogonal to the electric field of the first beam of RF energy and a second path of propagation, for passing the first beam of RF energy through said means and for reflecting the second beam of RF energy; and (b) means, disposed in the path of the first and the second beam of RF energy, for rotating the electric field of the first beam in a direction by 45° and for rotating the electric field of the second beam of RF energy in a similar direction by 45°.

Claim 14

The radar seeker as recited in claim 10 further comprising second means, disposed in the path of propagation of the first and the second beams of RF energy for reflecting the path of the first and the second beam of RF energy and for passing a third beam of RF energy through said second means.

Claim 15

The radar seeker as recited in claim 11 further comprising means, disposed in the path of propagation of the first, the second and the third beams of RF energy, for changing the second and the third beams of RF energy from circular polarization to linear polarization and for changing the first beam of RF energy from linear polarization to circular polarization.

Claim 16

The radar seeker as recited in claim 12 further comprising a plurality of lens disposed in the path of the first beam of RF energy.

Claim 17

A radar comprising (a) means for providing a first beam of linearly polarized radio frequency (RF energy; (b) diplexer means having a first, a second, a third and a fourth port, such diplexer means being responsive to the first beam incident on the first port, for converting the first beam to an initially convergent beam of circularly polarized RF energy out of the second port and, also being responsive to a second divergent beam of circularly polarized RF energy reflected from targets and incident on the second port, for converting in accordance with the direction of polarization of the RF energy in the second divergent beam, said energy to a second and a third beam of linearly polarized RF energy out of a respective one of the third and fourth ports; and (c) antenna means, responsive to the initially convergent beam of circularly polarized RF energy out of the second port and to RF energy reflected from targets, for collimating and directing the initially convergent beam of circularly polarized RF energy out of the second port and for providing the second divergent beam of circularly polarized RF energy.

Claim 18

A radar comprising (a) means for providing a first beam of linearly polarized radio frequency (RF energy; (b) diplexer means having a first, a second, a third and a fourth port, such diplexer means being responsive to the first beam incident on the first port, for converting the first beam to an initially convergent beam of circularly polarized RF energy out of the second port and, also being responsive to a second divergent beam of circularly polarized RF energy reflected from targets and incident on the second port, for converting in accordance with the direction of polarization of the RF energy in the second divergent beam, said energy to a second and a third beam of linearly polarized RF energy out of a respective one of the third and fourth ports; and (c) antenna means, responsive to the initially convergent beam of circularly polarized RF energy out of the second port and to RF energy reflected from targets, for collimating and directing the initially convergent beam of circularly polarized RF energy out of the second port and for providing the second divergent beam of circularly polarized RF energy.

Claim 19

The radar as recited in claim 13 wherein the diplexer means comprises: (a) means, responsive to the first beam of linearly polarized RF energy having an electric field and a first path of propagation, for passing the first beam of linearly polarized RF energy through said means and responsive to a second beam of linearly polarized RF energy having an electric field orthogonal to the electric field of the first beam of linearly polarized RF energy and a second path of propagation, for reflecting the path of propagation of the second beam of linearly polarized RF energy; and (b) means, disposed in the path of the first and the second beams of linearly polarized RF energy by 45°.

Claim 20

The radar as recited in claim 14 wherein the diplexer means comprises second means, disposed in the path of propagation of the first and the second beams of linearly polarized RF energy for reflecting the path of the first and the second beams of linearly polarized RF energy and for passing the third beam of linearly polarized energy through said second means.

Claim 21

The radar as recited in claim 16 further comprising means, disposed in the path of propagation of the first, the second and the third beams of linearly polarized RF energy, for changing the second and the third beams of RF energy from circular polarization to linearly polarization and for changing the first beam of linearly polarized RF energy from linear polarization to circular polarization.

Claim 22

The radar as recited in claim 16 further comprising a plurality of lens disposed in the path of the first beam of linearly polarized RF energy.

Claim 25

The method as recited in claim 19 further comprising the step of reflecting the first radio frequency signal toward the focal plane of the antenna and the second radio frequency signal from the focal plane of the antenna.